+

WO2009038785A3 - Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication - Google Patents

Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication Download PDF

Info

Publication number
WO2009038785A3
WO2009038785A3 PCT/US2008/010932 US2008010932W WO2009038785A3 WO 2009038785 A3 WO2009038785 A3 WO 2009038785A3 US 2008010932 W US2008010932 W US 2008010932W WO 2009038785 A3 WO2009038785 A3 WO 2009038785A3
Authority
WO
WIPO (PCT)
Prior art keywords
portions
methods
making same
coating
engine
Prior art date
Application number
PCT/US2008/010932
Other languages
English (en)
Other versions
WO2009038785A2 (fr
Inventor
Anand Kulkarni
Original Assignee
Siemens Energy Inc
Anand Kulkarni
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Energy Inc, Anand Kulkarni filed Critical Siemens Energy Inc
Priority to EP08831952.0A priority Critical patent/EP2193216B1/fr
Publication of WO2009038785A2 publication Critical patent/WO2009038785A2/fr
Publication of WO2009038785A3 publication Critical patent/WO2009038785A3/fr

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249961—With gradual property change within a component
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

L'invention concerne un revêtement céramique destiné à conférer une ou plusieurs variétés de caractéristiques fonctionnelles (par ex. réduire les niveaux de vibrations) à une ou plusieurs pièces ou parties d'un moteur (par ex., des segments annulaires, des conduites de transition, des brûleurs, des pales, des aubes et des tôles de protection d'un moteur de turbine, des parties de ces pièces et des parties d'un moteur diesel), les pièces ou les parties comprenant ce revêtement, et leurs procédés de fabrication. Le revêtement céramique présente un gradient ou un autre changement de caractéristique(s) fonctionnelle(s) sur l'épaisseur du revêtement, sur la surface du revêtement ou sur les deux.
PCT/US2008/010932 2007-09-19 2008-09-19 Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication WO2009038785A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP08831952.0A EP2193216B1 (fr) 2007-09-19 2008-09-19 Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US97355407P 2007-09-19 2007-09-19
US97356307P 2007-09-19 2007-09-19
US60/973,563 2007-09-19
US60/973,554 2007-09-19
US12/019,931 US7846561B2 (en) 2007-09-19 2008-01-25 Engine portions with functional ceramic coatings and methods of making same
US12/019,931 2008-01-25

Publications (2)

Publication Number Publication Date
WO2009038785A2 WO2009038785A2 (fr) 2009-03-26
WO2009038785A3 true WO2009038785A3 (fr) 2009-06-04

Family

ID=40454776

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/US2008/010873 WO2009038749A1 (fr) 2007-09-19 2008-09-19 Conférer des caractéristiques fonctionnelles à des parties de moteur
PCT/US2008/010932 WO2009038785A2 (fr) 2007-09-19 2008-09-19 Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication

Family Applications Before (1)

Application Number Title Priority Date Filing Date
PCT/US2008/010873 WO2009038749A1 (fr) 2007-09-19 2008-09-19 Conférer des caractéristiques fonctionnelles à des parties de moteur

Country Status (3)

Country Link
US (2) US8153204B2 (fr)
EP (2) EP2193217B1 (fr)
WO (2) WO2009038749A1 (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8603930B2 (en) 2005-10-07 2013-12-10 Sulzer Metco (Us), Inc. High-purity fused and crushed zirconia alloy powder and method of producing same
US7723249B2 (en) * 2005-10-07 2010-05-25 Sulzer Metco (Us), Inc. Ceramic material for high temperature service
US8153204B2 (en) * 2007-09-19 2012-04-10 Siemens Energy, Inc. Imparting functional characteristics to engine portions
DE102008002572A1 (de) * 2008-06-20 2009-12-24 Federal-Mogul Nürnberg GmbH Verfahren zur Herstellung eines Kolbens für einen Verbrennungsmotor sowie Kolben für einen Verbrennungsmotor
US9011104B2 (en) 2010-01-06 2015-04-21 General Electric Company Articles having damping coatings thereon
US9273400B2 (en) * 2010-05-24 2016-03-01 Sikorsky Aircraft Corporation Multilayered coating for improved erosion resistance
US20120177908A1 (en) * 2010-07-14 2012-07-12 Christopher Petorak Thermal spray coatings for semiconductor applications
US20120183790A1 (en) * 2010-07-14 2012-07-19 Christopher Petorak Thermal spray composite coatings for semiconductor applications
AU2012362827B2 (en) 2011-12-30 2016-12-22 Scoperta, Inc. Coating compositions
US20130171367A1 (en) * 2011-12-30 2013-07-04 Grzegorz Jan Kusinski Coating compositions, applications thereof, and methods of forming
DE102012200491B4 (de) 2012-01-13 2015-05-28 Lufthansa Technik Ag Gasturbinenschaufel für ein Flugzeugtriebwerk und Verfahren zur Beschichtung einer Gasturbinenschaufel
US20140220324A1 (en) * 2012-08-15 2014-08-07 Christopher W. Strock Thermal barrier coating having outer layer
CN104870753B (zh) 2012-12-20 2017-03-15 西门子公司 带有MCrAlY涂层和隔热涂层补片的燃气轮机导叶组件
US9816392B2 (en) 2013-04-10 2017-11-14 General Electric Company Architectures for high temperature TBCs with ultra low thermal conductivity and abradability and method of making
US10132185B2 (en) * 2014-11-07 2018-11-20 Rolls-Royce Corporation Additive process for an abradable blade track used in a gas turbine engine
KR102447682B1 (ko) * 2015-05-29 2022-09-27 삼성전자주식회사 코팅층 형성 방법, 플라즈마 처리 장치 및 패턴 형성 방법
CA2997367C (fr) 2015-09-04 2023-10-03 Scoperta, Inc. Alliages resistant a l'usure sans chrome et a faible teneur en chrome
US10145252B2 (en) * 2015-12-09 2018-12-04 General Electric Company Abradable compositions and methods for CMC shrouds
US10900371B2 (en) 2017-07-27 2021-01-26 Rolls-Royce North American Technologies, Inc. Abradable coatings for high-performance systems
US10858950B2 (en) 2017-07-27 2020-12-08 Rolls-Royce North America Technologies, Inc. Multilayer abradable coatings for high-performance systems
US11021989B2 (en) 2018-07-18 2021-06-01 Raytheon Technologies Corporation Environmental barrier multi-phase abradable coating
CA3117043A1 (fr) 2018-10-26 2020-04-30 Oerlikon Metco (Us) Inc. Alliages a base de nickel resistants a la corrosion et a l'usure
EP3947571B1 (fr) 2019-03-28 2024-05-22 Oerlikon Metco (US) Inc. Alliages à base de fer pour projection à chaud destinés au revêtement d'alésages de moteur
CA3136967A1 (fr) 2019-05-03 2020-11-12 Oerlikon Metco (Us) Inc. Charge d'alimentation pulverulente destinee au soudage en vrac resistant a l'usure, concue pour optimiser la facilite de production
CN111519125B (zh) * 2020-05-28 2022-03-29 广东省科学院新材料研究所 一种航空发动机涡轮外环的表面处理方法及航空发动机涡轮外环
CN111795984B (zh) * 2020-06-22 2022-05-10 中国科学院上海硅酸盐研究所 一种用于扫描电镜观察陶瓷内部微观结构的制样方法
US11866379B2 (en) 2020-08-14 2024-01-09 Rtx Corporation Hafnon and zircon environmental barrier coatings for silicon-based components

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3758233A (en) * 1972-01-17 1973-09-11 Gen Motors Corp Vibration damping coatings
EP1580293A2 (fr) * 2004-03-23 2005-09-28 Rolls-Royce PLC article ayant un revetement amortissant les vibrations et procede de formation d'un revetement amortissant les vibrations sur un article
EP1772441A1 (fr) * 2005-10-07 2007-04-11 Sulzer Metco (US) Inc. Matériau céramique et revêtements pour des applications à haute température

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2786779A (en) * 1953-02-09 1957-03-26 Dewrance & Co Method and apparatus for powdered metal deposition by oxy-fuel gas flame
US6102656A (en) * 1995-09-26 2000-08-15 United Technologies Corporation Segmented abradable ceramic coating
US6447848B1 (en) * 1995-11-13 2002-09-10 The United States Of America As Represented By The Secretary Of The Navy Nanosize particle coatings made by thermally spraying solution precursor feedstocks
US20010055652A1 (en) * 1999-12-17 2001-12-27 William John Dalzell Method of making abradable seal having improved properties
US6620525B1 (en) * 2000-11-09 2003-09-16 General Electric Company Thermal barrier coating with improved erosion and impact resistance and process therefor
US6716539B2 (en) * 2001-09-24 2004-04-06 Siemens Westinghouse Power Corporation Dual microstructure thermal barrier coating
CA2571099C (fr) 2005-12-21 2015-05-05 Sulzer Metco (Us) Inc. Methode et appareil hybrides de pulverisation a froid avec plasma
US8153204B2 (en) * 2007-09-19 2012-04-10 Siemens Energy, Inc. Imparting functional characteristics to engine portions

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3758233A (en) * 1972-01-17 1973-09-11 Gen Motors Corp Vibration damping coatings
EP1580293A2 (fr) * 2004-03-23 2005-09-28 Rolls-Royce PLC article ayant un revetement amortissant les vibrations et procede de formation d'un revetement amortissant les vibrations sur un article
EP1772441A1 (fr) * 2005-10-07 2007-04-11 Sulzer Metco (US) Inc. Matériau céramique et revêtements pour des applications à haute température
US20070082131A1 (en) * 2005-10-07 2007-04-12 Sulzer Metco (Us), Inc. Optimized high purity coating for high temperature thermal cycling applications

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
HAN ET AL: "A comparison of thermal shock behavior between currently plasma spray and supersonic plasma spray CeO2-Y2O3-ZrO2 graded thermal barrier coatings", SURFACE AND COATINGS TECHNOLOGY, ELSEVIER, AMSTERDAM, NL, vol. 201, no. 9-11, 31 January 2007 (2007-01-31), pages 5253 - 5256, XP005738647, ISSN: 0257-8972 *

Also Published As

Publication number Publication date
US20090074961A1 (en) 2009-03-19
WO2009038749A1 (fr) 2009-03-26
WO2009038785A2 (fr) 2009-03-26
US7846561B2 (en) 2010-12-07
US20090075057A1 (en) 2009-03-19
EP2193217B1 (fr) 2018-06-13
EP2193217A1 (fr) 2010-06-09
EP2193216A2 (fr) 2010-06-09
EP2193216B1 (fr) 2016-11-30
US8153204B2 (en) 2012-04-10

Similar Documents

Publication Publication Date Title
WO2009038785A3 (fr) Parties de moteur avec revêtements céramiques fonctionnels et leurs procédés de fabrication
EP2092163A4 (fr) Ensemble d'aubes configurées pour faire tourner un écoulement dans un moteur de turbine à gaz, un composant de stator comprenant l'ensemble d'aubes, une turbine à gaz et un moteur à réaction d'avion
DE60316513D1 (de) Fluggasturbinentriebwerk mit Kontrolleitschaufel für gegenläufige Niederdruckturbine
EP2230382A3 (fr) Etage de rotor de turbine à gaz
PL2099582T3 (pl) Urządzenie i sposób naprawy lub wytwarzania końców łopatek turbiny gazowej, w szczególności silnika lotniczego
WO2008128322A3 (fr) Diffuseur avec résistance améliorée à l'érosion
BR112012005997A2 (pt) artigos que incluem um substrato poroso que tem uma camada conformal sobre os mesmos
GB0504576D0 (en) Turbine blades and methods for depositing an erosion resistant coating on the same
TW200626787A (en) Airfoil with large fillet and micro-circuit cooling
GB2452515B (en) Seal coating between rotor blade and rotor disk slot in gas turbine engine
EP2390465A3 (fr) Composant de turbine à gaz avec des trous de refroidissement par film d'air ayant forme de chevron et procédés relatifs à celui-ci
EP1898051B8 (fr) Aube de turbine à gaz avec refroidissement du bord d'attaque
DE602004016065D1 (de) Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
BRPI0503610A (pt) ajuste do fluxo de ar em um componente de turbina através do depósito de uma camada metálica de revestimento
GB2436708B (en) Auxiliary gas turbine engine assembly, aircraft component and controller
SG125103A1 (en) Aluminide coating of gas turbine engine blade
PL2137381T3 (pl) Sposób wytwarzania powlekanych łopatek wirnika turbiny
BRPI0917586A2 (pt) dispositivo de amortecimento vibratório para uma pá de turbomáquina, turbomáquina, motor de turbina a gás e motor com hélices rápidas
DE502004006868D1 (de) Gasturbine, insbesondere flugtriebwerk
DE602005007116D1 (de) Turbinenlaufschaufel und Rotor eines Gasturbinentriebwerks mit solchen Schaufeln
WO2014042724A3 (fr) Pointe d'aube de compresseur de turbine résistant au transfert de métal
WO2009094171A3 (fr) Injecteur de carburant et son procédé d'assemblage
FR2895742B1 (fr) Systeme stratifie a phase pyrochlore
WO2008006960A3 (fr) Raccord entre pieces de matiere composite d ' un turbomoteur pour aeronef
WO2013102135A3 (fr) Moteur à turbine à gaz et aube de turbine

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08831952

Country of ref document: EP

Kind code of ref document: A2

REEP Request for entry into the european phase

Ref document number: 2008831952

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2008831952

Country of ref document: EP

NENP Non-entry into the national phase

Ref country code: DE

点击 这是indexloc提供的php浏览器服务，不要输入任何密码和下载